Aircraft Description
N355ST is a 1948 Cessna 195, a single-engine reciprocating (piston) aircraft registered to Scootair LLC in Alburgh, VT. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on September 23, 1998. The registration certificate was issued on September 1, 2017. The registration is set to expire on September 30, 2027. Powered by a Jacobs R755A SERIES engine producing 300 horsepower, N355ST is. The aircraft's Mode S transponder code is A3F902 (hex), used for ADS-B identification and flight tracking. The FAA registry record for N355ST was last updated on March 17, 2023. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The Cessna 195, Cessna's only postwar radial-engine aircraft, established new standards for business aviation in the late 1940s. First flown on July 15, 1947, it was a high-wing monoplane powered by a 300-horsepower Jacobs radial engine with five-seat capacity. With its distinctive all-aluminum construction and strutless wing design, the 195 offered performance superior to contemporary light aircraft. Cessna Aircraft Company manufactured 1,180 total aircraft in the 190/195 series from 1947 to 1954. AviatorDB tracks 80,556 Cessna aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is C195.
AviatorDB has found no NTSB accident or incident reports involving N355ST. AviatorDB cross-references all FAA registration data with NTSB accident and incident reports, providing a comprehensive safety overview for every registered aircraft in the United States.
Registered Owner
Powerplant & Avionics
NTSB Accident History (2)
| Date | NTSB # | Damage | Highest Injury | Probable Cause |
|---|---|---|---|---|
| Jun 28, 2005 | CHI05CA157 | Substantial | Minor | The pilot not maintaining directional control during the landing and the ground loop he encountered. |
| Jul 19, 2003 | CHI03LA222 | Substantial | None | The failure of the left main landing gear axle resulting in the brake being locked and subsequent loss of directional control. |
The pilot not maintaining directional control during the landing and the ground loop he encountered.
The failure of the left main landing gear axle resulting in the brake being locked and subsequent loss of directional control.
Additional Details
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-05-01 01:32:20 UTC